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Tables of stiffness and carry-over factor for flat rectangular plates under compression
National Advisory Committee for Aeronautics.
Tables of stiffness and carry-over factor are presented for infinitely long flat plates subjected to a uniformly distributed longitudinal compressive load. The tables are intended for use in solving problems in the stability of structures composed of plates under compression.
Originally issued as NACA as Advance Restricted Report L3K27 (November 1943).
Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia.
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Washington, D.C. : National Advisory Committee for Aeronautics, [1943]
Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L398